Flight mechanics/Navigation/Control/...
Robust model predictive control for satellite orbit maintenance using Hall effect thrusters

masumeh kiantaj; Morteza Farhid; Moharram Shameli

Articles in Press, Accepted Manuscript, Available Online from 10 December 2023

Abstract
  In this article, a robust model predictive controller is designed for maintaining the satellite's orbit in the low earth orbit. The designed control system makes it possible for the satellite to automatically keep the orbital parameters within the allowed range without the intervention of the ground ...  Read More

Flight mechanics/Navigation/Control/...
Two-Level Optimal Controller Design Based on PSO and Adaptive Control for Satellite Simulator System

Alireza Ahangarani Farahani; Reza Yaghoi; Seyed Majid Hosseini

Articles in Press, Accepted Manuscript, Available Online from 29 January 2024

Abstract
  In this paper, to control the Euler angles of a three-degree-of-freedom satellite simulator platform with uncertain parameters an adaptive inverse dynamic control method based on the PSO algorithm is presented. The design of the controller is done in two steps, in the first step, the control coefficients ...  Read More

Flight mechanics/Navigation/Control/...
Design of robust sliding mode controller for nonlinear chaotic gyroscope system with input saturation

Ali Foroutan; Alireza Safa

Articles in Press, Accepted Manuscript, Available Online from 21 January 2024

Abstract
  The gyroscope system is an attractive and efficient nonlinear system that is used in various military, aerospace, navigation, and many other important industries. In this paper, a robust sliding mode controller is proposed to control the chaotic gyroscope nonlinear system in the presence of noise, external ...  Read More

Flight mechanics/Navigation/Control/...
Air target tracking by homing missile using deep learning and fuzzy adaptive control

mohamad mahdi soori; seyed hosein Sadati

Articles in Press, Accepted Manuscript, Available Online from 29 January 2024

Abstract
  In the integrated guidance and control approach, the guidance law is developed separately and tested assuming the ideality of the autopilot. The autopilot is also designed independently and is tested assuming the ideality of the guidance law. This article describes the process of designing and simulating ...  Read More

Flight mechanics/Navigation/Control/...
A review of the application of optimization algorithms nature inspired in the design of flight paths

Iman Shafieenejad; Mohammadreza Banitalebi Dehkordi; Mohammad Amin Nourianpour

Volume 8, Issue 3 , September 2024, , Pages 75-99

https://doi.org/10.22034/jtae.2024.8.3.6

Abstract
  In this article, an overview of the application of optimization algorithms inspired by nature in the design of the flight path has been discussed. The significant increase in the capabilities and availability of independent ground and air tools makes safety and security challenges especially important ...  Read More

Flight mechanics/Navigation/Control/...
Integrated guidance and control of the Pitch channel in a homing missile using optimal linear and nonlinear model predictive control

mohamad mahdi soori; seyed hosein Sadati

Volume 8, Issue 2 , June 2024, , Pages 27-43

https://doi.org/10.22034/jtae.2024.8.2.3

Abstract
  This article describes the process of designing and simulating the performance of the predictive controller of the optimal model, which was created in order to guide the missile in a two-dimensional problem of minimizing the collision time and the distance from the target. In the design of the optimal ...  Read More

Flight mechanics/Navigation/Control/...
Automatic Mass Balancing of Spacecraft Attitude Simulator by Parameter Estimation and Linear Control

M. Barati; Mehdi Sabzehparvar; M. Navabi

Volume 8, Issue 2 , June 2024, , Pages 55-65

https://doi.org/10.22034/jtae.2024.8.2.5

Abstract
  In order to perform attitude control ground experiments, it is crucial to ensure the center of mass of the platform is coincident with the center of rotation as accurate as possible. In this paper, a linearized dynamic model of the imbalanced attitude platform is derived and a linear controller is methodically ...  Read More

Flight mechanics/Navigation/Control/...
Designing Pitch Angle Compensator for an UAV and Robustification it with Bee Colony Optimization Algorithm

Mohammad Hosein Alizadeh; Alireza Toloei

Volume 8, Issue 1 , April 2024, , Pages 1-14

https://doi.org/10.22034/jtae.2024.8.1.1

Abstract
  The intended aircraft in this issue is an UAV type, capable of performing multiple missions. In this paper, after the linearization of the pitch channel, the transfer function for important points is extracted. After that, a robust classic compensator and an angular velocity damper are designed. According ...  Read More

Flight mechanics/Navigation/Control/...
Formation control of unmanned helicopters using the sliding mode controller method

Fatemeh Ghaderi; Alireza Toloei; Reza Ghasemi

Volume 7, Issue 4 , January 2024, , Pages 11-21

https://doi.org/10.30699/jtae.2023.7.4.2

Abstract
  This article aims to control the group flight of unmanned helicopters. After presenting the dynamic equations using the Newton-Euler method, the dynamic inversion control has been applied to control the position and attitude of helicopters. generalized predictive control was also used to control the ...  Read More

Flight mechanics/Navigation/Control/...
Intelligent Tuning PID Controller, Simulation and Comparison for a Quadrotor

Mana Ghanifar; Milad Kamzan; Morteza Tayefi

Volume 7, Issue 4 , January 2024, , Pages 23-33

https://doi.org/10.30699/jtae.2023.7.4.3

Abstract
  n this paper, the use of PID controller to control a model of a quadrotor with nonlinear dynamics is investigated. In this regard, after presenting the designed nonlinear dynamic quadrotor model, four distinct methods for adjusting the parameters of this controller are examined and compared. These four ...  Read More

Flight mechanics/Navigation/Control/...
Using Neural Network to Estimate the Success Percent of Spacecraft Active Fault-Tolerant Controller

Rouzbeh Moradi; Jamila Hamzeyee

Volume 7, Issue 2 , June 2023, , Pages 11-16

https://doi.org/10.30699/jtae.2023.7.2.2

Abstract
  Determining the controller success percent is one of the important issues in spacecraft active fault-tolerant control. The importance of this subject is mainly related to the random and unpredictable nature of faults. On the other hand, since there exists a wide range of faults, various simulations and ...  Read More

Flight mechanics/Navigation/Control/...
Optimal Technology Allocation of in the Life Support Subsystem with Maximum Reliability

Milad Mahmoudi; A. B. Basohbate Novinzadeh; Farshad Pazooki

Volume 7, Issue 2 , June 2023, , Pages 29-37

https://doi.org/10.30699/jtae.2023.7.2.4

Abstract
  The atmosphere of the Red Planet or Mars contains 95% of carbon dioxide, 3% of nitrogen, 1.6% of argon and only a small amount of oxygen, and in terms of concentration is about one percent of the planet's atmosphere, which makes it virtually impossible for humans to live and survive on Mars. Therefore, ...  Read More

Flight mechanics/Navigation/Control/...
Distributed Intelligent Adaptive Sliding Mode Formation Protocol Design for Non-affine Nonlinear Multi-Agent Systems with UAV Application

pejman manouchehri,; reza ghasemi; Alireza toloui,

Volume 6, Issue 3 , October 2022, , Pages 21-31

https://doi.org/10.22034/jtae.2022.163673

Abstract
  due to the variability and uncertainty of some process parameters under investigation and limited uncertainties and confusions, the controller design faces problems. the controller is performed locally using the information of neighboring agents and the corresponding graph has a spanning tree. fuzzy ...  Read More

Flight mechanics/Navigation/Control/...
Development process of aircraft turbine engine control systems

Hojat Taie; Reza Gholamian; sepideh Ayati

Volume 6, Issue 3 , October 2022, , Pages 45-55

https://doi.org/10.22034/jtae.2022.163674

Abstract
  The performance of the propulsion system and the engine, known as the heart of the aircraft, is highly dependent on subsystems, such as the engine control subsystem.Today, most modern military and civil aircraft use turbine engines to generate thrust. The engine control system is one of the most challenging ...  Read More

Flight mechanics/Navigation/Control/...
Design of a Mobile-based Flying Robots

G Kahe; N. Karimi; M. Hamzehpour; A. Ghaderi

Volume 6, Issue 1 , June 2022, , Pages 7-15

https://doi.org/10.22034/jtae.2022.129736

Abstract
  The growth and use of smartphones have become a pervasive issue in many countries. On the other hand, one of the new and applied technologies that have been able to attract many enthusiasts is the civilian vertical drones or multi-rotors. The diverse and sometimes unique capabilities of flying robots ...  Read More

Flight mechanics/Navigation/Control/...
Robust H∞ Control Design for Thrust Vectoring System of a UAV

Hojat Taei; Ali Aboutalebiyan

Volume 6, Issue 1 , June 2022, , Pages 17-28

https://doi.org/10.22034/jtae.2022.273718.1166

Abstract
  The design of a controller for a thrust vector control system of UAV has been studied through the robust  H∞ control method. In the first, the governing space-state equations of the system have been derived using the bond graph approach. Then, the critical performance parameters of the system ...  Read More

Flight mechanics/Navigation/Control/...
Review of Re-entry Guidance Methods Based on Trajectory Generation

Reza Esmaelzadeh; fateme zahra rahmani

Volume 5, Issue 4 , February 2022, , Pages 61-72

https://doi.org/10.22034/jtae.2022.145235

Abstract
  One of the most important and complex issues in the field of aerospace engineering is the returning to the atmosphere. Many flying objects do not experience returning to the atmosphere. The study of this topic is relevant only to those flying objects that have left the atmosphere and their return to ...  Read More

Flight mechanics/Navigation/Control/...
Investigation of Changes in Structural Simulation of Three-axis Gyroscopic Stabilizer

Hamid Reza Moghaddas; Ali Mahmoodi; Farshad Pazooki

Volume 5, Issue 3 , November 2021, , Pages 1-19

https://doi.org/10.22034/jtae.2021.143406

Abstract
  A new approach is presented for the management of controlling the changes in design process of a triaxis gyroscopic stabilizer for a camera mounted on a flying robot. It includes decision-making and the way of identifying the best Investigation of the control process. As a prototype, the Phantom Flying ...  Read More

Flight mechanics/Navigation/Control/...
Model Predictive Control Based on Intelligent Model for Low Earth Orbit Satellite

Taha Yasini; Jafar Roshanian; Shahin Darvishpour

Volume 4, Issue 4 , February 2021, , Pages 31-41

Abstract
  In this paper, an orbit control algorithm is implemented for low earth orbit (LEO) satellites, using artificial neural networks (ANN), model-based predictive control (MPC), and linear quadratic regulator (LQR). As a self-tuning regulator structure, an ANN is used to learn the model of the satellite with ...  Read More